United States
15
2014-12-04
SNECMA from , US has applied for patents for these inventions. The list has both pending applications and granted patents:
Device for measuring vibration amplitudes of the blade tips in a turbomachine
#2 | 2014-11-06Propulsion assembly and method
#3 | 2014-09-25Airplane including means for taking at least a portion of the boundary layer of the flow of air over a surface
#4 | 2014-07-31Annular casing for a turbine engine compressor
#5 | 2013-12-05System for attaching a turbojet engine spinner
#6 | 2013-11-21METHOD FOR BONDING MANUFACTURING INTERMEDIARY PARTS, REFERRED TO AS IPS, TO A TURBOMACHINE BLADE MADE OF COMPOSITE MATERIAL
#7 | 2013-10-24AIRCRAFT PROPULSION ASSEMBLY
#8 | 2013-10-17Blade having an integrated composite spar
#9 | 2013-08-29System for detecting the first signs of a malfunction of an aircraft engine valve
#10 | 2013-08-29Device for lubricating an epicycloidal reduction gear
#11 | 2013-08-29METHOD OF MANUFACTURING A COMPOSITE PART BY INJECTING RESIN INTO A TOOL, AND DEVICE COMPRISING THIS TOOL
#12 | 2013-08-15Method for measuring the deformation of a turbo-machine blade during operation of the turbo-machine
#13 | 2013-08-15Annular anti-wear shim for a turbomachine
#14 | 2013-08-15Composite coupling with a machining portion
#15 | 2013-08-15Method for defining the shape of a turbomachine convergent-divergent nozzle, and corresponding convergent-divergent nozzle
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